Pressure distribution of aerofoils if embedded supersonic region

Ramaswamy, MA and Parikh, PC (1975) Pressure distribution of aerofoils if embedded supersonic region. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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Abstract

An exploratory attempt at empirically determining the pressure distribution on aerofoils in the embedded supersonic region using the concept of 'Expansion angle sand 'Compression angle ' in the flow development and the concept of connected points, both put forward by Pearcey (l), has been presented Prediction of the pressure distribution over the initial region is based on an universal compression rate curve and that over the region beyond it is based on an empirical correlation for the connected regions.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Airfoil embedded supersonics
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Users 90 not found.
Date Deposited: 14 Sep 2006
Last Modified: 24 May 2010 04:20
URI: http://nal-ir.nal.res.in/id/eprint/2717

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